Using optically filtered high-speed imaging to characterise expansion tube operating conditions
Author:
Funder
Australian Research Council
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-020-00948-x.pdf
Reference65 articles.
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2. Gildfind, D.E., Jacobs, P.A., Morgan, R.G., Chan, W.Y.K., Gollan, R.J.: Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling. Shock Waves 28(4), 877–897 (2018). https://doi.org/10.1007/s00193-017-0785-x
3. Gildfind, D.E., Jacobs, P.A., Morgan, R.G., Chan, W.Y.K., Gollan, R.J.: Scramjet test flow reconstruction for a large-scale expansion tube, part 2: axisymmetric CFD analysis. Shock Waves 28(4), 899–918 (2018). https://doi.org/10.1007/s00193-017-0786-9
4. Abul-Huda, Y.M., Gamba, M.: Flow characterization of a hypersonic expansion tube facility for supersonic combustion studies. J. Propul. Power 33(6), 1504–1519 (2017). https://doi.org/10.2514/1.B36543
5. Olivier, H.: An improved method to determine free stream conditions in hypersonic facilities. Shock Waves 3(2), 129–139 (1993). https://doi.org/10.1007/BF02115892
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